Abstract Redlich-Kwong-Peng-Robinson (RK-PR) was developed in recent years as a
promising generalized cubic equation of state (EoS) to allow for a good representation of …

In this paper, the trans-/near-/supercritical jet models were established using a combination
of large eddy numerical simulations and real fluid equations of state (EOS) in order to …

Increasing application of supercritical fluids leads to increased use of numerical simulations
to guide designs. However, the impact of Equations of State (EoS) selection on …

A pintle injector is a convenient method for adjusting propellant combustion and has
received extensive attention in recent years. However, few studies have examined the …

In this research, numerical simulation of three-phase flow (airflow, sulfide concentrate
particles, and liquid fuel droplets) within a copper flash smelting furnace was conducted to …

Combustion of cryogenic propellants is of great technological interest for researchers and
scientists nowadays. Due to high specific impulse, the use of liquid oxygen and hydrogen as …

To study the influence of injection time and injection volume on the working process of a two-
stroke kerosene direct injection engine, an experimental study was carried out on an …

Combustion chamber modeling and simulation of the liquid propellant engine with kerosene
as fuel and liquid oxygen as an oxidizer in the turbulent flow field are performed by CFD …

This study investigates the combustion characteristics of n-dodecane under pure oxygen
conditions, a critical scenario for rocket propulsion systems. Advanced laser absorption …

In recent years, LOX-Methane propellant combination has attracted lot of attention because
of its various advantages compared to typical LOX-Hydrogen rocket engines. ISRO is …